# Airworthiness Directives; SOCATAGroupe Aerospatiale Model TBM 700 Airplanes
> **Rule** · Final rule. · Published 1998-11-24 · Effective 1998-12-28 · 63 FR 64844
## Document
- **Document number:** 98-31010
- **Category:** airworthiness
- **Manufacturer:** SOCATAGroupe Aerospatiale Model TBM 700
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 63 FR 64844
- **Publication date:** 1998-11-24
- **Effective date:** 1998-12-28
- **FAA docket:** Docket No. 95-CE-65-AD
## Abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain SOCATA--Groupe AEROSPATIALE (SOCATA) Model TBM 700 airplanes. This AD requires repetitively inspecting (using visual methods) the web of the left and right flap carriage for cracks, and replacing any cracked flap carriage with one of improved design. The proposed AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for France. The actions specified by this AD are intended to detect and correct cracks in a flap carriage, which could result in loss of the flap function with consequent reduced and/or loss of airplane control.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/1998/11/24/98-31010/airworthiness-directives-socatagroupe-aerospatiale-model-tbm-700-airplanes)
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